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公开(公告)号：US10220228B2
公开(公告)日：2019-03-05
申请号：US15209985
申请日：2016-07-14
摘要： A fire suppression system for a plurality of enclosures in an aircraft comprises a plurality of bottles containing fire suppression agent, a temperature sensor and a pressure sensor on each bottle for measuring temperature and pressure data of the bottle contents, an addressable bottle valve on each bottle and a control unit. The control unit is configured to analyze the temperature and pressure data for each bottle to determine adequacy of fire suppression agent content for extinguishing a fire in a particular enclosure of the aircraft. The control unit is further configured to control the bottle valves independently by using the bottle valves' addresses, in order to manage the release of fire suppression agent.
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公开(公告)号：US20170014657A1
公开(公告)日：2017-01-19
申请号：US15209985
申请日：2016-07-14
CPC分类号： A62C3/08 , A62C35/13 , A62C37/44 , A62C99/0018 , B64D2045/009
摘要： A fire suppression system for a plurality of enclosures in an aircraft comprises a plurality of bottles containing fire suppression agent, a temperature sensor and a pressure sensor on each bottle for measuring temperature and pressure data of the bottle contents, an addressable bottle valve on each bottle and a control unit. The control unit is configured to analyse the temperature and pressure data for each bottle to determine adequacy of fire suppression agent content for extinguishing a fire in a particular enclosure of the aircraft. The control unit is further configured to control the bottle valves independently by using the bottle valves' addresses, in order to manage the release of fire suppression agent.
摘要翻译： 用于飞行器中的多个外壳的灭火系统包括在每个瓶上装有防火剂，温度传感器和压力传感器的多个瓶子，用于测量瓶子内容物的温度和压力数据，每个瓶子上的可寻址瓶阀 和控制单元。 控制单元被配置为分析每个瓶子的温度和压力数据，以确定用于扑灭飞机的特定外壳中的火焰的灭火剂含量的充分性。 控制单元进一步构造成通过使用瓶阀的地址独立地控制瓶阀，以便管理灭火剂的释放。
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公开(公告)号：US10195469B2
公开(公告)日：2019-02-05
申请号：US15209960
申请日：2016-07-14
摘要： A directional valve for a fire suppression system comprises a valve member for controlling the discharge of fire suppression agent. The valve member comprises: a blocking portion to provide a closed setting for the fire suppression agent; a first orifice to provide a fully open setting for the fire suppression agent; and a second orifice to provide a restricted opening setting in which discharge of fire suppression agent is restricted. The valve member is configured so that during activation of the directional valve from a closed setting, the first orifice follows the blocking portion and precedes the second orifice in order to provide a fully open setting followed by a restricted opening setting.
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公开(公告)号：US20170014656A1
公开(公告)日：2017-01-19
申请号：US15209960
申请日：2016-07-14
CPC分类号： A62C3/08 , A62C35/68 , A62C37/36 , A62C99/0018 , B64C19/00 , B64D45/00 , B64D2045/009
摘要： A directional valve for a fire suppression system comprises a valve member for controlling the discharge of fire suppression agent. The valve member comprises: a blocking portion to provide a closed setting for the fire suppression agent; a first orifice to provide a fully open setting for the fire suppression agent; and a second orifice to provide a restricted opening setting in which discharge of fire suppression agent is restricted. The valve member is configured so that during activation of the directional valve from a closed setting, the first orifice follows the blocking portion and precedes the second orifice in order to provide a fully open setting followed by a restricted opening setting.
摘要翻译： 用于灭火系统的方向阀包括用于控制灭火剂排放的阀构件。 阀构件包括：阻挡部分，用于为灭火剂提供封闭的设置; 为防火剂提供完全开启的设置的第一孔口; 以及第二孔口，用于限制灭火剂的排放受到限制的开启设置。 阀构件被构造成使得在从闭合设置激活方向阀时，第一孔遵循阻挡部分并且在第二孔口之前，以提供完全打开的设置，然后是受限制的开启设置。
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公开(公告)号：US20170014655A1
公开(公告)日：2017-01-19
申请号：US15209936
申请日：2016-07-14
CPC分类号： A62C3/08 , A62C35/13 , A62C37/36 , A62C99/0018 , B64C19/00 , B64D45/00 , B64D2045/009 , G08B17/10
摘要： An aircraft has a fire suppression control system for a plurality of enclosures within the aircraft. The aircraft comprises a directional valve for each enclosure, sensors provided for each enclosure, for monitoring variables of the enclosure, one or more fire suppression agent bottles and a control unit for regulating the discharge of the fire suppression agent. The sensors are operatively linked by the control unit to a warning system in a cockpit of the aircraft.
摘要翻译： 飞机具有用于飞行器内的多个外壳的灭火控制系统。 飞机包括用于每个外壳的换向阀，为每个外壳设置的传感器，用于监控外壳的变量，一个或多个灭火剂瓶和用于调节灭火剂排放的控制单元。 传感器通过控制单元可操作地连接到飞行器驾驶舱中的警告系统。
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